EP3409399B1 - Nozzle structure - Google Patents
Nozzle structure Download PDFInfo
- Publication number
- EP3409399B1 EP3409399B1 EP16888102.7A EP16888102A EP3409399B1 EP 3409399 B1 EP3409399 B1 EP 3409399B1 EP 16888102 A EP16888102 A EP 16888102A EP 3409399 B1 EP3409399 B1 EP 3409399B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- nozzle
- inner bore
- refractory
- sleeve
- bore sleeve
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D41/00—Casting melt-holding vessels, e.g. ladles, tundishes, cups or the like
- B22D41/50—Pouring-nozzles
- B22D41/502—Connection arrangements; Sealing means therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D41/00—Casting melt-holding vessels, e.g. ladles, tundishes, cups or the like
- B22D41/50—Pouring-nozzles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/10—Supplying or treating molten metal
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D41/00—Casting melt-holding vessels, e.g. ladles, tundishes, cups or the like
- B22D41/50—Pouring-nozzles
- B22D41/52—Manufacturing or repairing thereof
- B22D41/54—Manufacturing or repairing thereof characterised by the materials used therefor
Definitions
- the present invention relates to a nozzle structure for discharging molten steel.
- a nozzle structure as a molten steel discharge path from a molten steel inlet port to a casting mold may comprise a refractory body ("nozzle body") which is divided into a plurality of refractory members ("nozzle members”) in a direction orthogonal to a direction of discharge of molten steel (upward-downward direction).
- a nozzle structure in which the flow rate control function is performed not by a nozzle body, but by a stopper 7 provided at a top of the nozzle body, wherein the nozzle body is formed as an integral immersion nozzle with no joint.
- a casting time tends to extend for a long time due to multi-sequential continuous casting or the like, so that, in order to replace a part of the nozzle structure such as an immersion nozzle or the like, a nozzle body comprising a plurality of divided refractory members (nozzle members) may still be required in some cases. In such a case, joints should still be present.
- Patent Document 1 discloses the following invention:
- JP S5786063 and JP 2002 153970 are related to nozzle structures for discharging molten metal having an inner bore sleeve comprising one or more non-continuous recesses or continuous grooves provided on an outer periphery of the inner sleeve.
- Patent Document 1 gas-sealing is performed by introducing the gas (inert gas), so that the risk of drawing the outside air, or oxygen which is particularly harmful to the molten steel can be reduced.
- the gas (inert gas) is still drawn.
- gas (inert gas) is drawn, various problems associated with oxidation of molten steel and refractory body is reduced, but there still remains a risk that quality defects such as pinholes may be caused in the steel.
- the problem to be solved by the present invention is to improve sealing performance in a nozzle structure for discharging molten steel which comprises a plurality of refractory members and one or more joints.
- the present invention provides nozzle structures 1 to 7 as below.
- the nozzle structure comprising an inner bore sleeve provided on an inner bore surface of the nozzle structure body so as to extend across at least one of the joints in the upward-downward direction, can achieve an enhanced sealing performance. Further, the nozzle structure comprising an inner bore sleeve which is provided so as to extend across all of the joints in the upward-downward direction, can achieve the same degree of sealing performance as an integral nozzle structure with no joint.
- the inner bore sleeve has the recesses or the grooves on the outer periphery thereof, so that even in the case of breaking and detaching the nozzle member at a specific location of the nozzle structure, it is possible to securely and accurately separate the nozzle member at a given portion without harming the sealing property. Thereafter, even in the case of attaching the replacement article, it is possible to reduce the unevenness of the joining surface and maintain the joining precision at a high level, and to easily perform the detachment and attachment work of the nozzle member.
- the nozzle structure of the present invention makes it possible to freely and easily select and apply refractories having various materials and physical properties, which are different in damages on the inner bore surface and characteristics of deposition of alumina inclusions and the like.
- a typical embodiment of a nozzle structure of the present invention having the largest number of divisions or number of joints comprises a refractory body (nozzle body) which comprised of a plurality of refractory members (nozzle members) such as an upper nozzle, a sliding nozzle plate of three layers (upper plate, middle plate, lower plate), an middle nozzle, a lower nozzle, and an immersion nozzle.
- nozzle body which comprised of a plurality of refractory members (nozzle members) such as an upper nozzle, a sliding nozzle plate of three layers (upper plate, middle plate, lower plate), an middle nozzle, a lower nozzle, and an immersion nozzle.
- nozzle body which comprised of a plurality of refractory members (nozzle members) such as an upper nozzle, a sliding nozzle plate of three layers (upper plate, middle plate, lower plate), an middle nozzle, a lower nozzle, and an immersion nozzle.
- nozzle members such as an upper nozzle, a sliding nozzle plate of three layers (upper plate,
- Figure 1 (a) depicts an embodiment of a nozzle structure comprising an upper nozzle 1, an upper plate 2a, a middle plate 2b, a lower plate 2c, a lower nozzle 3, and an immersion nozzle 4
- Figure 1 (b) depicts an embodiment of a nozzle structure comprising an upper nozzle 1 and an immersion nozzle 4.
- the present invention provides a nozzle structure for discharging molten steel, wherein the nozzle structure comprises: a molten steel discharge path having an inner bore 5; and one or more joints through which the molten steel discharge path is divided at one or more positions in a orthogonal direction with respect to an upward-downward direction of discharge of molten steel, and which join the molten steel discharge path.
- the nozzle structure of the present invention further comprises an inner bore sleeve 6 formed of a refractory material, and provided on an inner bore surface of the nozzle structure to extend in the upward-downward direction across at least one of the joints.
- the inner bore sleeve 6 ensures sealing performance of the nozzle structure.
- the inner bore sleeve 6 is formed as an integral structure without dividing it in a direction orthogonal to an upward-downward direction, and then is provided so as to extend across all of the joints in the upward-downward direction.
- the inner bore sleeve provided so as to extend across at least one of the joints in the upward-downward direction can also contribute to an enhanced sealing performance.
- the inner bore sleeve 6 may be divided into a plurality of pieces in a direction orthogonal to an upward-downward direction.
- the divided portion i.e., a joint A1 of the inner sleeve from being aligned with the divided portions, i.e., joints B1 and B2 of the molten steel discharge path, which is a nozzle body of the nozzle structure.
- the description that the inner bore sleeve is provided to extend across the joints in the upward-downward direction means that the inner bore sleeve is a continuous body in which the inner bore sleeve is not divided in the upward-downward direction at a position opposed to each of the one or more joints in a direction orthogonal to the upward-downward direction.
- an offset distance in the upward-downward direction between the joint A1 of the inner bore sleeve 6 and the joins B1, B2 of the nozzle body is empirically preferably greater than or equal to a thickness of the inner bore sleeve 6.
- each of the nozzle members (refractory member) constituting the nozzle structure accurately exists at a given position in a direction orthogonal to the upward-downward direction.
- the given position for each nozzle member is determined by a set of the nozzle members or the like.
- the inner bore sleeve 6 typically has a cylindrical shape as shown in FIG. 4 , preferably, the upper end on the inner bore side thereof has a curved or inclined surface as shown in FIG. 5 , that is, has an angle as small as possible or a gradually-increasing shape with respect to the discharge direction of the molten steel. If the inner bore sleeve has a large-angled stepped structure such as a surface in the direction orthogonal to the discharge direction of the molten steel, the flow of the molten steel is greatly disturbed at that portion, and as the result, adhesion of inclusions, local damage of the inner bore sleeve or the like can occur.
- an inner bore surface 6a of the inner bore sleeve 6 can be flush with the inner bore surface 5a of the nozzle structure. This allows the stepped portions of the inner bore surfaces at the upper end and a lower end of the inner bore sleeve 6 to eliminate.
- the inner bore surface 5a of the nozzle structure near the lower end of the inner bore sleeve 6 may be provided with a protruding portion and an inclined portion.
- the inner bore sleeve 6 may be provided with one or more non-continuous recesses 6b or continuous grooves 6c on an outer periphery thereof.
- the inner bore sleeve 6 may be provided with one or more non-continuous recesses 6b or continuous grooves 6c on an outer periphery thereof.
- four separated recesses 6b are provided on a part of the outer periphery of the inner bore sleeve 6, and in an embodiment of Figure 10 , a continuous groove 6c in a circumferential direction is provided on a part of the outer periphery of the inner bore sleeve 6.
- the recesses 6b and the continuous groove 6c are provided on the outer periphery of the inner bore sleeve 6 at a position opposed to each of the joints of the nozzle body in the orthogonal direction.
- the reason for the above is as follows. First, in the case of detaching the immersion nozzle 4 at a position of the joining surface on the upper end thereof as shown in FIG. 11 , for example, in the event of emergency or for replacing a part of the refractory members (parts) of the nozzle structure, if the inner bore sleeve 6 is attached inside the nozzle, the inner bore sleeve 6 may be broken at an irregular position in a complicated form, and breakage itself may be difficult to perform.
- the inner bore sleeve 6 can be easily broken, and further can be broken with high accuracy from a desired predetermined position (see Figure 12 ).
- the above “emergency” includes a case where an abnormality occurs in the stopper control, so that the nozzle is closed at a location other than the stopper in order to stop the molten steel flow, for example, a case where a part of the nozzle structure is slidable and the inner bore sleeve is broken and removed at a sliding portion by sliding.
- the above “replacing a part of the refractory members (parts) of the nozzle structure” includes, for example, a case where the immersion nozzle is slid in a direction orthogonal (orthogonal direction) to an upward-downward direction or a mechanical load is applied diagonally downward to the immersion nozzle, thereby breaking the bore sleeve and detaching the immersion nozzle, and after sliding another new immersion nozzle in the orthogonal direction or attaching it from below.
- the inner sleeve can be easily broken with high precision and little unevenness.
- an area of the recesses or continuous grooves which are arranged on at least one of front and back surfaces of the inner bore sleeve along a sliding direction of a nozzle or along a pressure-applied direction for disassembling and removing the nozzle below the joints is greater than that of the remaining recesses or continuous grooves. This is because the outer periphery portion of the outer sleeve along the sliding direction or the pressure-applied direction becomes the origin of the stress.
- the inner bore sleeve 6 is provided on the inner bore surface of the nozzle structure via an adhesive.
- an adhesive is necessary to take measures such as enhancing the surface accuracy of the joining surface to the extent that gas does not pass through. This is impractical measures in terms of cost.
- the adhesive can be used without particular limitation as long as it is a material generally used for a nozzle structure, such as a material which does not cause melting or the like depending on the composition of the nozzle structure. According to empirical knowledge of the inventors of the present invention, for example, when mortar having an apparent porosity of about 30% or less after heat treatment at a temperature of about 1000 °C to 1400 °C is used, gas or the like may not pass through to the inner bore.
- deposition or growth of non-metallic inclusions such as alumina or metals on the inner bore surface of the inner sleeve 6 adversely affects the quality and productivity of the steel in operation, such as disturbance of the flow of molten steel during casting and reduction of casting speed. Furthermore, it is difficult to disassemble or detach the nozzle members including the immersion nozzle. Then, the material of the inner bore sleeve 6 is designed to have higher anti-deposition capability than a refractory material of the nozzle body of the nozzle structure, thereby making it possible to reduce deposition of alumina inclusions and the like onto the inner bore surface, and more to reduce deposition or growth of metal on it.
- the material having high anti-deposition capability includes a refractory material containing about 15 mass % or more of a CaO component and a remainder including refractory components such as MgO, ZrO2, and Carbon, wherein a mass ratio of CaO/MgO is the range of 0.1 to 1.5; material containing or adjusting the chemical composition that reacts with other molten steel and components in the molten steel to smooth the surface; or material with improved surface smoothness.
- the nozzle structure for discharging the molten steel from the tundish to the mold has been illustrated herein as an example, the present invention is not limited to the use for the tundish, and may be applied to other nozzle structures for discharging the molten steel.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Casting Support Devices, Ladles, And Melt Control Thereby (AREA)
- Continuous Casting (AREA)
Description
- The present invention relates to a nozzle structure for discharging molten steel.
- For example, for discharging molten steel from a tundish, a nozzle structure as a molten steel discharge path from a molten steel inlet port to a casting mold may comprise a refractory body ("nozzle body") which is divided into a plurality of refractory members ("nozzle members") in a direction orthogonal to a direction of discharge of molten steel (upward-downward direction).
- In the nozzle structure in which the plurality of refractory members are combined, one or more joints are inevitably present between the refractory members. For the nozzle member involving sliding such as sliding nozzle, the joints cannot be used with joint filling material and sealant, so that they have a contact structure, which are so-called "dry joints". And for other nozzle members without sliding, the joints are often provided with mortar or sealing material. However, even in varying degrees depending on the presence or absence of the joint filling material and the like, outside air is prone to be drawn into an inner bore of the nozzle structure from the joints (see
Figure 13 ). When the outside air is drawn, there are caused depositing or clogging of alumina inclusions or the like on or in the inner bore, increase in oxides, quality deterioration of other steels, etc. - As solution to drawing of the outside air, as shown in
Figure 14 , for example, it is possible to adopt a nozzle structure in which the flow rate control function is performed not by a nozzle body, but by astopper 7 provided at a top of the nozzle body, wherein the nozzle body is formed as an integral immersion nozzle with no joint. However, in continuous casting of steel, a casting time tends to extend for a long time due to multi-sequential continuous casting or the like, so that, in order to replace a part of the nozzle structure such as an immersion nozzle or the like, a nozzle body comprising a plurality of divided refractory members (nozzle members) may still be required in some cases. In such a case, joints should still be present. - As solution to drawing of the outside air at the joints,
Patent Document 1 discloses the following invention: - a casting nozzle which comprises a refractory nozzle body for the casting nozzle and a case provided on an outer periphery of the refractory nozzle body, wherein a metal pipe having a plurality of gas blowing holes or slits is provided in a gap formed between the refractory nozzle body and the case so as to cover at least a portion of the outer periphery or an inner periphery of the refractory nozzle body, and wherein a gas is introduced from at least one end of the metal pipe through the gas blowing holes or slits to thereby gas-seal a peripheral vicinity of the refractory nozzle body.
-
JP 2007 229798 A -
JP H07 51839 A -
US 2013/334263 A1 is related to a refractory product comprising CaO component-containing refractory particles and MgO component-containing refractory particles. The refractory product contains, in terms of a chemical composition measured after it has undergone heating in a non-oxidizing atmosphere at 1000 °C, one or more metal oxides selected from the group consisting of B2O3, TiO2, V2O5, P2O5 and SiO2 in a total amount of 0.1 to 5.0 mass %, and free carbon in an amount of 2 to 35 mass %, with the remainder including CaO and MgO whose mass ratio (CaO/MgO) is in the range of 0.1 to 1.5. A casting nozzle comprising the refractory product formed in a multi-layer structure comprises first refractory layer and a second refractory layer. -
JP S5786063 JP 2002 153970 -
- [Patent Document 1]
JPH11-104814A - [Patent Document 2]
JP 2007 229798 A - [Patent Document 3]
JP H07 51839 A - [Patent Document 4]
US 2013/334263 A1 - [Patent Document 5]
JP S57 86063 - [Patent Document 6]
JP 2002 153970 A - In
Patent Document 1, gas-sealing is performed by introducing the gas (inert gas), so that the risk of drawing the outside air, or oxygen which is particularly harmful to the molten steel can be reduced. However, the gas (inert gas) is still drawn. Thus, when gas (inert gas) is drawn, various problems associated with oxidation of molten steel and refractory body is reduced, but there still remains a risk that quality defects such as pinholes may be caused in the steel. - The problem to be solved by the present invention is to improve sealing performance in a nozzle structure for discharging molten steel which comprises a plurality of refractory members and one or more joints.
- The present invention provides
nozzle structures 1 to 7 as below. - 1. A nozzle structure for discharging molten steel, wherein the nozzle structure comprises:
- a nozzle body having a molten steel discharge path therein, and comprising a plurality of nozzle refractory members arranged to divide the molten steel discharge path at one or more positions in an orthogonal direction with respect to an upward-downward direction and joined together through one or more joints, wherein at least one of the nozzle refractory members is configured to be detachable through a sliding movement in an orthogonal direction thereof or application of a mechanical load applied diagonally downward to the at least one nozzle refractory member during casting operation; and
- an inner bore sleeve formed of a refractory material, and provided on an inner bore surface of the nozzle body to extend in the upward-downward direction across at least one of the joints which joins said at least one detachable nozzle refractory member and an adjacent one of the remaining nozzle refractory members.
- 2. The nozzle structure as described in above 1, wherein the inner bore sleeve is provided on the inner bore surface via an adhesive.
- 3. The nozzle structure as described in above 1 or 2, wherein an inner bore-side upper end of the inner bore sleeve has a curved or inclined surface.
- 4. The nozzle structure as described in any of above 1 to 3, wherein the inner bore sleeve comprises one or more non-continuous recesses or continuous grooves provided on an outer periphery of the inner bore sleeve at a position opposed to each of the one or more joints in the orthogonal direction.
- 5. The nozzle structure as described in above 4, among the one or more non-continuous recesses or continuous grooves, an area of the recesses or continuous grooves which are arranged on at least one of front and back surfaces of the inner bore sleeve along a sliding direction of a nozzle or along a pressure-applied direction for disassembling and removing the nozzle below the joints, is relatively greater than that of the remaining recesses or continuous grooves.
- 6. In an unclaimed embodiment, the nozzle structure as described in any of above 1 to 5, the refractory material of the inner bore sleeve has higher anti-deposition capability than that of a nozzle body of the nozzle structure.
- 7. The nozzle structure as described in above 5 , wherein the inner bore sleeve is composed of a refractory material containing about 15 mass % or more of a CaO component and a remainder including MgO, wherein a mass ratio of CaO/MgO is the range of 0.1 to 1.5.
- According to the present invention, the nozzle structure comprising an inner bore sleeve provided on an inner bore surface of the nozzle structure body so as to extend across at least one of the joints in the upward-downward direction, can achieve an enhanced sealing performance. Further, the nozzle structure comprising an inner bore sleeve which is provided so as to extend across all of the joints in the upward-downward direction, can achieve the same degree of sealing performance as an integral nozzle structure with no joint.
- Further, the inner bore sleeve has the recesses or the grooves on the outer periphery thereof, so that even in the case of breaking and detaching the nozzle member at a specific location of the nozzle structure, it is possible to securely and accurately separate the nozzle member at a given portion without harming the sealing property. Thereafter, even in the case of attaching the replacement article, it is possible to reduce the unevenness of the joining surface and maintain the joining precision at a high level, and to easily perform the detachment and attachment work of the nozzle member.
- Moreover, the nozzle structure of the present invention makes it possible to freely and easily select and apply refractories having various materials and physical properties, which are different in damages on the inner bore surface and characteristics of deposition of alumina inclusions and the like.
-
-
Figure 1 is a conceptual view of an embodiment of a nozzle structure of the present invention, wherein:Figure 1 (a) depicts an example of the nozzle structure comprising an upper nozzle, an upper plate, a middle plate, a lower plate, a lower nozzle, and an immersion nozzle, andFigure 1 (b) depicts an example of the nozzle structure comprising an upper nozzle, and an immersion nozzle. -
Figure 2 is a conceptual view of an embodiment of a nozzle structure of the present invention, wherein joints through which the molten steel discharge path is divided at one or more positions in a orthogonal direction with respect to an upward-downward direction of discharge of molten steel and which join the molten steel discharge path, do not coincide with joints of an inner bore sleeve in terms of a position in the upward-downward direction. -
Figure 3 is a conceptual view of an embodiment of a nozzle structure of the present invention, wherein a nozzle (refractory member) provided at relatively lower side has a notch in the upper end of an inner bore surface of the nozzle, that is, it has an inclined or curved surface downward toward the inner bore side. -
Figure 4 is a conceptual view of an embodiment of an inner bore sleeve of the present invention, wherein:Figure 4 (a) depicts a top plan view thereof, andFigure 4 (b) depicts a longitudinal sectional view thereof. -
Figure 5 is a conceptual longitudinal sectional view of an embodiment of an inner bore sleeve of the present invention, wherein an inner side (inner bore-side) upper end of the inner bore sleeve has a curved or inclined surface. -
Figure 6 is a conceptual view of an embodiment of a nozzle structure of the present invention, wherein an inner bore surface of the inner bore sleeve attached inside the nozzle structure is flush with an inner bore surface of the nozzle structure. -
Figure 7 is a conceptual longitudinal sectional view of an embodiment of a nozzle structure of the present invention, wherein the inner bore surface of the inner bore sleeve attached inside the nozzle structure is only at the lower end thereof, flush with the inner bore surface of the nozzle structure. -
Figure 8 is a conceptual longitudinal sectional view of an embodiment of an inner bore sleeve of the present invention, wherein one or separated recesses or one groove are/is provided on a part of the outer periphery of the inner bore sleeve. -
Figure 9 is a conceptual view from A - A section ofFigure 8 , wherein four separated recesses are provided on a part of the outer periphery of the inner bore sleeve inFigure 8 . -
Figure 10 is a conceptual view from A - A section ofFigure 8 , wherein a continuous groove in a circumferential direction is provided on a part of the outer periphery of the inner bore sleeve inFigure 8 . -
Figure 11 is a conceptual view, of an embodiment of the nozzle structure ofFigure 1(a) wherein the inner bore sleeve is broken and then the immersion nozzle is detached at the upper end of joining surface, and of an embodiment in the case where the inner bore sleeve is attached in the region from the molten steel inlet port to the upper end of the immersion nozzle. -
Figure 12 is a conceptual longitudinal sectional view of an embodiment of a nozzle structure of the present invention, in a case where a new immersion nozzle is attached after detaching the immersion nozzle as inFigure 2 . -
Figure 13 is a conceptual view of, an embodiment of a nozzle structure having joints comprising a conventional upper nozzle, a sliding nozzle plate having a three-layer structure, a lower nozzle and an immersion nozzle, and an embodiment in the case where outside air is drawn from the joints. -
Figure 14 is a conceptual view of an embodiment of an integral structure nozzle (immersion nozzle) with no joint. - A typical embodiment of a nozzle structure of the present invention having the largest number of divisions or number of joints comprises a refractory body (nozzle body) which comprised of a plurality of refractory members (nozzle members) such as an upper nozzle, a sliding nozzle plate of three layers (upper plate, middle plate, lower plate), an middle nozzle, a lower nozzle, and an immersion nozzle. However, the present invention should be not limited to this embodiment, but may be any of the embodiments in which any two or more of the respective refractory members (nozzle members) are combined. For example,
Figure 1 (a) depicts an embodiment of a nozzle structure comprising anupper nozzle 1, anupper plate 2a, amiddle plate 2b, alower plate 2c, alower nozzle 3, and animmersion nozzle 4, andFigure 1 (b) depicts an embodiment of a nozzle structure comprising anupper nozzle 1 and animmersion nozzle 4. More specifically, the present invention provides a nozzle structure for discharging molten steel, wherein the nozzle structure comprises: a molten steel discharge path having aninner bore 5; and one or more joints through which the molten steel discharge path is divided at one or more positions in a orthogonal direction with respect to an upward-downward direction of discharge of molten steel, and which join the molten steel discharge path. The nozzle structure of the present invention further comprises aninner bore sleeve 6 formed of a refractory material, and provided on an inner bore surface of the nozzle structure to extend in the upward-downward direction across at least one of the joints. - The
inner bore sleeve 6 ensures sealing performance of the nozzle structure. In order to further enhance the sealing performance, most preferably, theinner bore sleeve 6 is formed as an integral structure without dividing it in a direction orthogonal to an upward-downward direction, and then is provided so as to extend across all of the joints in the upward-downward direction. However, the inner bore sleeve provided so as to extend across at least one of the joints in the upward-downward direction, can also contribute to an enhanced sealing performance. - Further, as shown in
Figure 2 , theinner bore sleeve 6 may be divided into a plurality of pieces in a direction orthogonal to an upward-downward direction. However, in the case of such a divided configuration, it is necessary to prevent the divided portion, i.e., a joint A1 of the inner sleeve from being aligned with the divided portions, i.e., joints B1 and B2 of the molten steel discharge path, which is a nozzle body of the nozzle structure. In other words, as used in the present invention, the description that the inner bore sleeve is provided to extend across the joints in the upward-downward direction, means that the inner bore sleeve is a continuous body in which the inner bore sleeve is not divided in the upward-downward direction at a position opposed to each of the one or more joints in a direction orthogonal to the upward-downward direction. Moreover, in order to effectively suppress drawing of outside air (gas) from an outside of the nozzle structure, an offset distance in the upward-downward direction between the joint A1 of theinner bore sleeve 6 and the joins B1, B2 of the nozzle body is empirically preferably greater than or equal to a thickness of theinner bore sleeve 6. - Further, when attaching the inner bore sleeve, it is necessary that each of the nozzle members (refractory member) constituting the nozzle structure accurately exists at a given position in a direction orthogonal to the upward-downward direction. The given position for each nozzle member is determined by a set of the nozzle members or the like. However, as shown in
Figure 3 , for example, at the upper end of the inner bore surface of the nozzle member attached relatively below, it is preferable to provide a notch having a length equal to or greater than the relative accuracy in the orthogonal direction between the upper nozzle member and the lower nozzle member, that is, a portion having an inclined or curved surface downward toward the inner bore side. Thus, when inserting the inner bore sleeve from above into the inner bore of the nozzle structure, the inner sleeve can be smoothly attached. - Although the
inner bore sleeve 6 typically has a cylindrical shape as shown inFIG. 4 , preferably, the upper end on the inner bore side thereof has a curved or inclined surface as shown inFIG. 5 , that is, has an angle as small as possible or a gradually-increasing shape with respect to the discharge direction of the molten steel. If the inner bore sleeve has a large-angled stepped structure such as a surface in the direction orthogonal to the discharge direction of the molten steel, the flow of the molten steel is greatly disturbed at that portion, and as the result, adhesion of inclusions, local damage of the inner bore sleeve or the like can occur. - As shown in
Figure 6 , aninner bore surface 6a of theinner bore sleeve 6 can be flush with theinner bore surface 5a of the nozzle structure. This allows the stepped portions of the inner bore surfaces at the upper end and a lower end of theinner bore sleeve 6 to eliminate. - As shown in
Figure 7 , it is also possible to eliminate the stepped portion of the inner bore surface only at the lower end of theinner bore sleeve 6. This stepped portion at the lower end can also serve as a base point at which disturbance of the flow of molten steel such as vortex occurs at this portion. In such a case, it is possible to suppress the turbulence of the molten steel flow even by merely eliminating the stepped portion of the inner bore surface only at the lower end of theinner bore sleeve 6. Further, by setting the lower end of theinner bore sleeve 6 to have the same diameter as theinner bore surface 5a of the nozzle body (to be flush with theinner bore surface 5a), it is possible to prevent theinner bore sleeve 6 from falling downward or slipping downward. Furthermore, in order to prevent theinner bore sleeve 6 from falling downward or slipping downward, theinner bore surface 5a of the nozzle structure near the lower end of theinner bore sleeve 6 may be provided with a protruding portion and an inclined portion. - As shown in
Figure 8 , theinner bore sleeve 6 may be provided with one or morenon-continuous recesses 6b orcontinuous grooves 6c on an outer periphery thereof. For example, in an embodiment ofFigure 9 , four separatedrecesses 6b are provided on a part of the outer periphery of theinner bore sleeve 6, and in an embodiment ofFigure 10 , acontinuous groove 6c in a circumferential direction is provided on a part of the outer periphery of theinner bore sleeve 6. Therecesses 6b and thecontinuous groove 6c are provided on the outer periphery of theinner bore sleeve 6 at a position opposed to each of the joints of the nozzle body in the orthogonal direction. The reason for the above is as follows. First, in the case of detaching theimmersion nozzle 4 at a position of the joining surface on the upper end thereof as shown inFIG. 11 , for example, in the event of emergency or for replacing a part of the refractory members (parts) of the nozzle structure, if theinner bore sleeve 6 is attached inside the nozzle, theinner bore sleeve 6 may be broken at an irregular position in a complicated form, and breakage itself may be difficult to perform. Therefore, as described above, by providing therecesses 6b and thegroove 6c on the outer periphery of theinner bore sleeve 6 at a position opposed to each of the joints of the nozzle body in the orthogonal direction (in the case ofFigure 11 , at a position opposed to the upper end of theimmersion nozzle 4 in the orthogonal direction), theinner bore sleeve 6 can be easily broken, and further can be broken with high accuracy from a desired predetermined position (seeFigure 12 ). - The above "emergency" includes a case where an abnormality occurs in the stopper control, so that the nozzle is closed at a location other than the stopper in order to stop the molten steel flow, for example, a case where a part of the nozzle structure is slidable and the inner bore sleeve is broken and removed at a sliding portion by sliding. Further, the above "replacing a part of the refractory members (parts) of the nozzle structure" includes, for example, a case where the immersion nozzle is slid in a direction orthogonal (orthogonal direction) to an upward-downward direction or a mechanical load is applied diagonally downward to the immersion nozzle, thereby breaking the bore sleeve and detaching the immersion nozzle, and after sliding another new immersion nozzle in the orthogonal direction or attaching it from below. In any of these cases, preferably, the inner sleeve can be easily broken with high precision and little unevenness.
- Preferably, among the
recesses 6b and thegrooves 6c, an area of the recesses or continuous grooves which are arranged on at least one of front and back surfaces of the inner bore sleeve along a sliding direction of a nozzle or along a pressure-applied direction for disassembling and removing the nozzle below the joints, is greater than that of the remaining recesses or continuous grooves. This is because the outer periphery portion of the outer sleeve along the sliding direction or the pressure-applied direction becomes the origin of the stress. - Preferably, the
inner bore sleeve 6 is provided on the inner bore surface of the nozzle structure via an adhesive. Although providing theinner bore sleeve 6 reduces the risk of drawing of gas, in the case of not using the adhesive, it is necessary to take measures such as enhancing the surface accuracy of the joining surface to the extent that gas does not pass through. This is impractical measures in terms of cost. - The adhesive (mortar) can be used without particular limitation as long as it is a material generally used for a nozzle structure, such as a material which does not cause melting or the like depending on the composition of the nozzle structure. According to empirical knowledge of the inventors of the present invention, for example, when mortar having an apparent porosity of about 30% or less after heat treatment at a temperature of about 1000 °C to 1400 °C is used, gas or the like may not pass through to the inner bore.
- On the other hand, deposition or growth of non-metallic inclusions such as alumina or metals on the inner bore surface of the
inner sleeve 6 adversely affects the quality and productivity of the steel in operation, such as disturbance of the flow of molten steel during casting and reduction of casting speed. Furthermore, it is difficult to disassemble or detach the nozzle members including the immersion nozzle. Then, the material of theinner bore sleeve 6 is designed to have higher anti-deposition capability than a refractory material of the nozzle body of the nozzle structure, thereby making it possible to reduce deposition of alumina inclusions and the like onto the inner bore surface, and more to reduce deposition or growth of metal on it.
The material having high anti-deposition capability includes a refractory material containing about 15 mass % or more of a CaO component and a remainder including refractory components such as MgO, ZrO2, and Carbon, wherein a mass ratio of CaO/MgO is the range of 0.1 to 1.5; material containing or adjusting the chemical composition that reacts with other molten steel and components in the molten steel to smooth the surface; or material with improved surface smoothness. - Although, in the above embodiments, the nozzle structure for discharging the molten steel from the tundish to the mold has been illustrated herein as an example, the present invention is not limited to the use for the tundish, and may be applied to other nozzle structures for discharging the molten steel.
-
- 1:
- upper nozzle
- 2a:
- upper plate
- 2b:
- middle plate
- 2c:
- lower plate
- 3:
- lower nozzle
- 4:
- immersion nozzle
- 5:
- inner bore
- 5a:
- inner bore surface
- 6:
- inner bore sleeve
- 6a:
- inner bore surface
- 6b:
- recess
- 6c:
- groove
- 7:
- stopper
Claims (6)
- A nozzle structure for discharging molten steel, comprising:a nozzle body having a molten steel discharge path therein, and comprising a plurality of nozzle refractory members arranged to divide the molten steel discharge path at one or more positions in an orthogonal direction with respect to an upward-downward direction and joined together through one or more joints, wherein at least one of the nozzle refractory members is configured to be detachable through a sliding movement in an orthogonal direction thereof or application of a mechanical load applied diagonally downward to the at least one nozzle refractory member during casting operation; andan inner bore sleeve (6) formed of a refractory material, and provided on an inner bore surface (5a) of the nozzle body to extend in the upward-downward direction across at least one of the joints which joins said at least one detachable nozzle refractory member and an adjacent one of the remaining nozzle refractory members.
- The nozzle structure as recited in claim 1, wherein the inner bore sleeve (6) is provided on the inner bore surface (5a) via an adhesive.
- The nozzle structure as recited in claim 1 or 2, wherein an inner bore-side upper end of the inner bore sleeve (6) has a curved or inclined surface.
- The nozzle structure as recited in any one of claims 1 to 3, wherein the inner bore sleeve (6) comprises one or more non-continuous recesses (6b) or continuous grooves (6c) provided on an outer periphery of the inner bore sleeve (6) at a position opposed to each of the one or more joints in the orthogonal direction.
- The nozzle structure as recited in claim 4, among the one or more non-continuous recesses (6b) or continuous grooves (6c), an area of the recesses (6b) or continuous grooves (6c) which are arranged on at least one of front and back surfaces of the inner bore sleeve (6) along a sliding direction of a nozzle or along a pressure-applied direction for disassembling and removing the nozzle below the joints, is relatively greater than that of the remaining recesses (6b) or continuous grooves (6c).
- The nozzle structure as recited in any of claims 1 to 5, wherein the inner bore sleeve (6) is composed of a refractory material containing about 15 mass % or more of a CaO component and a remainder including MgO, wherein a mass ratio of CaO/MgO is the range of 0.1 to 1.5.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2016011775A JP6663230B2 (en) | 2016-01-25 | 2016-01-25 | Nozzle structure |
PCT/JP2016/083186 WO2017130517A1 (en) | 2016-01-25 | 2016-11-09 | Nozzle structure |
Publications (3)
Publication Number | Publication Date |
---|---|
EP3409399A1 EP3409399A1 (en) | 2018-12-05 |
EP3409399A4 EP3409399A4 (en) | 2019-08-14 |
EP3409399B1 true EP3409399B1 (en) | 2021-01-06 |
Family
ID=59397609
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP16888102.7A Active EP3409399B1 (en) | 2016-01-25 | 2016-11-09 | Nozzle structure |
Country Status (10)
Country | Link |
---|---|
US (1) | US10799950B2 (en) |
EP (1) | EP3409399B1 (en) |
JP (1) | JP6663230B2 (en) |
KR (1) | KR102132983B1 (en) |
CN (1) | CN108778564B (en) |
AU (1) | AU2016390149B2 (en) |
BR (1) | BR112018015149B1 (en) |
CA (1) | CA3011206C (en) |
TW (1) | TWI615220B (en) |
WO (1) | WO2017130517A1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP7182496B2 (en) * | 2019-03-12 | 2022-12-02 | 黒崎播磨株式会社 | Nozzle and structure of nozzle and stopper |
JP2021049564A (en) * | 2019-09-26 | 2021-04-01 | 黒崎播磨株式会社 | Tundish upper nozzle structure and method of continuous casting |
EP3827912B1 (en) * | 2019-11-26 | 2022-03-30 | Refractory Intellectual Property GmbH & Co. KG | An exchangeable nozzle for a nozzle changer system, a method for manufacturing such a nozzle, a nozzle changer system comprising such a nozzle and a tundish comprising such a nozzle changer system |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4165026A (en) * | 1971-12-07 | 1979-08-21 | Foseco Trading A.G. | Tundish with expendable lining and easily removable nozzle |
JPS5919789B2 (en) * | 1979-07-27 | 1984-05-08 | 新日本製鐵株式会社 | How to repair sliding nozzle |
JPS595489Y2 (en) * | 1980-11-12 | 1984-02-18 | 川崎製鉄株式会社 | Nozzle for molten metal injection |
JPS57134252A (en) * | 1981-02-10 | 1982-08-19 | Nippon Steel Corp | Nozzle for continuous casting |
US5348275A (en) * | 1993-07-26 | 1994-09-20 | Magneco/Metrel, Inc. | Tundish nozzle assembly block |
US5723055A (en) * | 1995-10-10 | 1998-03-03 | Vesuvius Crucible Company | Nozzle assembly having inert gas distributor |
JPH09220649A (en) * | 1996-02-09 | 1997-08-26 | Akechi Ceramics Kk | Long nozzle for continuous casting |
DE19818028C2 (en) | 1997-04-22 | 2001-11-29 | Toshiba Ceramics Co | Integrated immersion nozzle and process for its manufacture |
JPH115145A (en) * | 1997-04-22 | 1999-01-12 | Toshiba Ceramics Co Ltd | Integrated soak nozzle and manufacturing method thereof |
JPH11104814A (en) | 1997-10-01 | 1999-04-20 | Toshiba Ceramics Co Ltd | Nozzle for casting |
JP2002096145A (en) * | 2000-09-18 | 2002-04-02 | Nippon Steel Corp | Nozzle for continuous casting and continuous casting method of steel using the nozzle |
JP2002153970A (en) * | 2000-11-22 | 2002-05-28 | Shinagawa Refract Co Ltd | Multi-layer structural molten metal pouring nozzle |
DE60313446T2 (en) * | 2002-04-02 | 2008-07-24 | Krosakiharima Corp., Kitakyushu | BINDING STRUCTURE OF A FIRE-RESISTANT SLEEVE FOR THE INTERNAL HOLE OF A NOZZLE FOR CONTINUOUS CASTING |
DE602004022073D1 (en) * | 2003-08-22 | 2009-08-27 | Krosakiharima Corp | TUBE NOZZLE FOR STEEL STEELING AND STEEL STEELING METHOD USING THE DIVING NOZZLE |
JP4512560B2 (en) * | 2006-03-03 | 2010-07-28 | 新日本製鐵株式会社 | Continuous casting nozzle |
BRPI0916819B1 (en) | 2008-07-28 | 2018-03-06 | Nippon Steel & Sumitomo Metal Corporation | REFRACTORY MATERIAL FOR AN INTERMEDIATE LAYER OF A CONTINUOUS LANGUAGE NOZZLE AND A CONTINUOUS LANGUAGE NOZZLE |
JP5129684B2 (en) * | 2008-08-06 | 2013-01-30 | 黒崎播磨株式会社 | Continuous casting nozzle |
JP4695701B2 (en) * | 2009-07-24 | 2011-06-08 | 黒崎播磨株式会社 | Molten metal discharge nozzle |
JP2014512277A (en) * | 2011-04-29 | 2014-05-22 | ベスビウス クルーシブル カンパニー | Refractory elements, assemblies and tundish for transporting molten metal |
JP5830108B2 (en) * | 2011-12-01 | 2015-12-09 | 黒崎播磨株式会社 | Refractories and casting nozzles |
EP2977126B1 (en) * | 2013-03-21 | 2022-05-04 | Krosakiharima Corporation | Refractory material and nozzle for casting |
AR099467A1 (en) * | 2014-02-19 | 2016-07-27 | Vesuvius Group Sa | COAT SPOON COAT FOR METAL COAT, COUPLING ASSEMBLY SET TO COUPLING SUCH COVER SPOON COVERING TO A SPOON, METAL COATING INSTALLATION AND COUPLING PROCESS |
-
2016
- 2016-01-25 JP JP2016011775A patent/JP6663230B2/en not_active Expired - Fee Related
- 2016-11-09 EP EP16888102.7A patent/EP3409399B1/en active Active
- 2016-11-09 CA CA3011206A patent/CA3011206C/en active Active
- 2016-11-09 CN CN201680077658.XA patent/CN108778564B/en not_active Expired - Fee Related
- 2016-11-09 WO PCT/JP2016/083186 patent/WO2017130517A1/en active Application Filing
- 2016-11-09 BR BR112018015149-1A patent/BR112018015149B1/en not_active IP Right Cessation
- 2016-11-09 KR KR1020187018451A patent/KR102132983B1/en not_active Expired - Fee Related
- 2016-11-09 US US16/070,934 patent/US10799950B2/en not_active Expired - Fee Related
- 2016-11-09 AU AU2016390149A patent/AU2016390149B2/en not_active Ceased
- 2016-11-28 TW TW105139086A patent/TWI615220B/en not_active IP Right Cessation
Non-Patent Citations (1)
Title |
---|
None * |
Also Published As
Publication number | Publication date |
---|---|
US10799950B2 (en) | 2020-10-13 |
WO2017130517A1 (en) | 2017-08-03 |
EP3409399A4 (en) | 2019-08-14 |
CA3011206A1 (en) | 2017-08-03 |
BR112018015149B1 (en) | 2021-09-08 |
EP3409399A1 (en) | 2018-12-05 |
KR20180088871A (en) | 2018-08-07 |
CA3011206C (en) | 2020-05-05 |
US20190030599A1 (en) | 2019-01-31 |
JP6663230B2 (en) | 2020-03-11 |
AU2016390149A1 (en) | 2018-07-26 |
AU2016390149B2 (en) | 2020-03-19 |
KR102132983B1 (en) | 2020-07-10 |
CN108778564A (en) | 2018-11-09 |
BR112018015149A2 (en) | 2018-12-18 |
CN108778564B (en) | 2020-12-29 |
TW201731611A (en) | 2017-09-16 |
TWI615220B (en) | 2018-02-21 |
JP2017131902A (en) | 2017-08-03 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP3409399B1 (en) | Nozzle structure | |
EP3939717B1 (en) | Nozzle, and nozzle and stopper combination | |
US5954989A (en) | Erosion and abrasion resistant refractory composition and article made therefrom | |
US10183326B2 (en) | Slab continuous casting apparatus | |
EP1789220B1 (en) | Stopper rod for delivering gas into a molten metal | |
JP4139366B2 (en) | Molten metal discharge nozzle with function of blowing gas | |
JP2004136367A (en) | Joint structure of continuous casting nozzle having carbon-containing CaO-based refractory layer | |
JP6630157B2 (en) | Immersion nozzle | |
KR20080064428A (en) | Continuous Casting Stopper | |
EP2711107B1 (en) | Refractory ceramic gas purging plug and a process for manufacturing said gas purging plug | |
JP2010023057A (en) | Refractory for molten metal nozzle and method for preventing suction of air from crack part thereof | |
JPH11188463A (en) | Immersion nozzle for continuous casting | |
JPS63256249A (en) | Submerged nozzle for continuous casting | |
JP2005088021A (en) | Immersion nozzle | |
JPH06254663A (en) | Intermediate nozzle with insulating layer for continuous casting | |
JPH1058099A (en) | Tundish stopper for continuous casting | |
KR20160064552A (en) | Nozzle and method for producing the same | |
TWM504222U (en) | Oxygen lance |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE |
|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
17P | Request for examination filed |
Effective date: 20180820 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
DAV | Request for validation of the european patent (deleted) | ||
DAX | Request for extension of the european patent (deleted) | ||
A4 | Supplementary search report drawn up and despatched |
Effective date: 20190711 |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: B22D 11/10 20060101AFI20190705BHEP Ipc: B22D 41/50 20060101ALI20190705BHEP |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
17Q | First examination report despatched |
Effective date: 20200103 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
INTG | Intention to grant announced |
Effective date: 20200626 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 1351815 Country of ref document: AT Kind code of ref document: T Effective date: 20210115 Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602016051238 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: FP |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MK05 Ref document number: 1351815 Country of ref document: AT Kind code of ref document: T Effective date: 20210106 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG9D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210506 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210406 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210407 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210406 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210506 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602016051238 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 |
|
26N | No opposition filed |
Effective date: 20211007 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210506 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 602016051238 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20211109 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20211109 Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20211130 |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20211130 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20211109 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20211109 Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220601 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20211130 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 20221114 Year of fee payment: 7 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220701 Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20161109 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220701 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MM Effective date: 20231201 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20231201 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20231201 Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210106 |